Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:bypassRatio |
0.48:1
|
| gptkbp:compressionRatio |
single-shaft axial-flow
|
| gptkbp:countryOfOrigin |
gptkb:France
|
| gptkbp:diameter |
0.91 m
|
| gptkbp:firstFlight |
1970
|
| gptkbp:fuelType |
aviation kerosene
|
| gptkbp:intendedUse |
military fighter aircraft
|
| gptkbp:length |
4.96 m
|
| gptkbp:manufacturer |
gptkb:Snecma
|
| gptkbp:notableFeature |
modular design
|
| gptkbp:numberOfStages |
2
9 |
| gptkbp:status |
in service
|
| gptkbp:successor |
gptkb:Snecma_M88
|
| gptkbp:thrust |
95 kN
|
| gptkbp:type |
afterburning turbofan
|
| gptkbp:usedInAircraft |
gptkb:Dassault_Mirage_2000
Dassault Mirage 4000 |
| gptkbp:weight |
1,520 kg
|
| gptkbp:bfsParent |
gptkb:Mirage_2000EAD
|
| gptkbp:bfsLayer |
7
|
| http://www.w3.org/2000/01/rdf-schema#label |
Snecma M53 turbofan
|